WELCOME TO MOSES Rev devlop ============================ This Program is licensed for the exclusive use of Ultramarine inc. Copying of this program or use by anyone other than an employee of the above firm without written consent of Ultramarine is strictly prohibited. +++ M A I N +++ =============== >&device -g_default device -oecho no >inmodel *zp000 2 0 *zp010 1.969615 0.3472964 *zp020 1.879385 0.6840402 *zp030 1.732051 1 *zp040 1.532089 1.285575 *zp050 1.285575 1.532089 *zp060 1 1.732051 *zp070 0.6840406 1.879385 *zp080 0.3472966 1.969615 *zp090 3.894144E-7 2 *zp100 -0.3472958 1.969615 *zp110 -0.6840398 1.879385 *zp120 -1 1.732051 *zp130 -1.285575 1.532089 *zp140 -1.532088 1.285575 *zp150 -1.732051 1 *zp160 -1.879385 0.684041 *zp170 -1.969615 0.347297 *zp180 -2 7.788289E-7 *zp190 -1.969616 -0.3472956 *zp200 -1.879385 -0.6840394 *zp210 -1.732051 -0.9999993 *zp220 -1.532089 -1.285574 *zp230 -1.285576 -1.532088 *zp240 -1.000001 -1.73205 *zp250 -0.684041 -1.879385 *zp260 -0.3472972 -1.969615 *zp270 -9.298247E-7 -2 *zp280 0.3472954 -1.969616 *zp290 0.6840394 -1.879385 *zp300 0.9999991 -1.732052 *zp310 1.285574 -1.53209 *zp320 1.532088 -1.285576 *zp330 1.73205 -1.000001 *zp340 1.879385 -0.6840416 *zp350 1.969615 -0.3472978 Time To perform Inmodel : CP= 0.08 >&title Plate with Hole >&subtitle Original Mesh >&selec :p -sel *a@ *b@ *c@ *d@ *e@ *f@ >&channel gra -file hole.ans/ho_orig.eps >&pict top -type struct -poin :p -ano poin -color default >&summ +++ & S U M M A R Y +++ ======================= >plate >cat >end +++ M A I N +++ =============== +++ M O D E L E D I T I N G +++ ================================= +++ M A I N +++ =============== +++ M O D E L S I Z E +++ =========================== Number of Bodies = 1 Number of Parts = 2 Number of Compartments = 1 Number of Load Groups = 6 Number of Panels = 0 Number of Points = 2761 Number of Nodes = 2732 Number of Classes = 3 Number of Elements = 19 Number of Sub Elements = 5287 Number of Load Points = 21004 Number of Load Attributes = 0 Number of Load Cases = 0 +++ S T R U C T U R A L S O L U T I O N +++ ============================================= Generating Loads on TEST at Time 0.000 ====================================== Total Global Force -1200.00 0.00 0.00 0 0 0 Time To Generate Load Cases : CP= 0.03 Reducing Stiffness of DEFAULT ============================= Time to Define Model Topology : CP= 0.18 Time to Complete Nodal Loads : CP= 0.01 Time to Define Stiffness Blocks : CP= 0.01 Time to Form Element Matricies : CP= 0.28 Time to Form Global Stiffness Matrix : CP= 0.04 Time to Form Global Load Matrix : CP= 0.00 *** WARNING: 4.7 Sig. Figures Lost At **IN1427 In Direction Z ============================================================== Time to Factor Stiffness Matrix : CP= 1.22 Expanding Results of DEFAULT ============================ Time For Backward Substitution : CP= 0.00 Time to Store Deflections : CP= 0.01 Time to Store Element Internal Loads : CP= 0.09 +++ M A I N +++ =============== +++ S T R U C T U R A L P O S T - P R O C E S S I N G +++ =========================================================== +++ M A I N +++ =============== MOSES Finished Normally ========================= CP Time 3.12 ======================== Total Units 3.12 ========================